CN210515168U

CN210515168U - Fixing support of computer box for aerospace

Info

Publication number: CN210515168U
Application number: CN201922104445.5U
Authority: CN
Inventors: 霍慧娟; 屈思源
Original assignee: Shaanxi Juteng Precision Machinery Technology Co Ltd
Current assignee: Shaanxi Juteng Precision Machinery Technology Co Ltd
Priority date: 2019-11-29
Filing date: 2019-11-29
Publication date: 2020-05-12
Anticipated expiration: 2029-11-29

Abstract

The utility model discloses a fixed bolster of computer box for aerospace, including first support and second support, through cutting formula connecting piece swing joint between first support and the second support, first support includes the bottom plate, the baffle, reinforcing plate and backup pad, the bottom plate links firmly with one side bottom of baffle perpendicularly, backup pad and baffle with the perpendicular fixed connection in one side upper end, the top of reinforcing plate and baffle, be connected with a plurality of elasticity post between backup pad and the bottom plate, a plurality of bar hole has evenly been seted up in the backup pad, it includes head rod and second connecting rod to cut the formula connecting piece, the upper end and the first support tip of head rod are articulated, the lower extreme and the second support tip of head rod are articulated, the upper end of second connecting rod is articulated with the tip of second support, the lower extreme of second connecting rod is articulated with the tip of first support. The utility model discloses can install not unidimensional quick-witted case, application scope is wide, increases the reliability of using and the stability of being connected.

Description

Fixing support of computer box for aerospace

Technical Field

The utility model relates to a machine case fixed technical field, in particular to fixed bolster of computer box for aerospace.

Background

The width design of the machine case of most computers on the market at present is narrower, and is not very firm when adopting vertical placement, topples over very easily when receiving external force collision, because the inside electron device of machine case is very easy to be damaged, and the machine case in case of toppling over will cause very big loss, except that can design the machine case fixed position on the special desk, all the other can not design special safeguard measure.

SUMMERY OF THE UTILITY MODEL

A primary object of the present invention is to provide a fixing bracket for an aerospace computer case, which can effectively solve the problems of the prior art.

In order to achieve the above purpose, the utility model adopts the following technical scheme:

a fixed support of a computer box for aerospace comprises a first support and a second support, wherein the first support is movably connected with the second support through a shear type connecting piece, the first support comprises a bottom plate, a baffle, a reinforcing plate and a supporting plate, the bottom plate is vertically and fixedly connected with the bottom of one side of the baffle, the supporting plate is vertically and fixedly connected with the upper end of the same side of the baffle, the reinforcing plate is arranged above the baffle, a plurality of elastic columns are connected between the supporting plate and the bottom plate, a plurality of strip-shaped holes are uniformly formed in the supporting plate, the shear type connecting piece comprises a first connecting rod and a second connecting rod which are mutually rotatably connected, the upper end of the first connecting rod is hinged with the end part of the first support, the lower end of the first connecting rod is hinged with the end part of the second support, and the upper end of the second connecting rod is hinged with the end part of the second support, the lower end of the second connecting rod is hinged with the end part of the first support.

Preferably, the first support and the second support have the same size.

Preferably, the reinforcing plates are two, the bottom of each reinforcing plate is fixedly connected with the same base plate, and the bottom ends of the base plates are provided with anti-skidding lines.

Preferably, the two side edges of the supporting plate are both vertically fixed with a limiting plate.

Preferably, the elastic column comprises a fixed sleeve, a spring and a loop bar, the bottom of the loop bar extends to the inner side of the sleeve and is connected with the upper end of the spring, and the lower end of the spring is connected with the bottom of the inner side of the sleeve.

Preferably, a rubber pad is fixed on the upper end surface of the baffle.

Compared with the prior art, the utility model discloses following beneficial effect has: the fixing support for the computer case for aerospace is characterized in that the case is clamped and fixed through the first support and the second support, the stability of the case is improved, the case is prevented from falling down by external force, the safety of the case is protected, loss is avoided, meanwhile, the support plate is arranged, the first support and the second support are movably connected through the shear type connecting piece, cases with different sizes can be installed according to the distance between the first support and the second support, the application range is wide, the case is installed on the support plate and can play a role in ventilating and radiating the bottom of the case, the elastic column is connected between the support plate and the bottom plate, the case is installed on the support plate, the weight of the case begins to be compressed towards the elastic column, so that the first connecting rod and the second connecting rod in the shear type connecting piece do not rotate relatively, and the first support and the second support do not move any more due to the anti-slip grains arranged at the bottom end of the, the reliability of use and the stability of connection can be increased, the safety of the case is guaranteed, and the use is more convenient.

Drawings

Fig. 1 is the utility model relates to an overall structure schematic diagram of the fixed bolster of computer box for aerospace.

Fig. 2 is the utility model relates to a structural schematic of the first support of computer box for aerospace.

Fig. 3 is the utility model discloses a cross-sectional view of the elasticity post of computer box for aerospace.

In the figure: 1. a first support; 2. a second support; 3. a scissor linkage; 4. a base plate; 5. a baffle plate; 6. a reinforcing plate; 7. a support plate; 8. an elastic column; 9. a strip-shaped hole; 10. a first connecting rod; 11. a second connecting rod; 12. a base plate; 13. a limiting plate; 14. fixing the sleeve; 15. a spring; 16. a sleeve barrel; 17. and (7) a rubber pad.

Detailed Description

In order to make the technical means, creation features, achievement purposes and functions of the present invention easy to understand, the present invention is further described below with reference to the following embodiments.

As shown in fig. 1-3, a fixed bolster of computer box for aerospace, includes first support 1 and second support 2, first support 1 with through cutting formula connecting piece 3 swing joint between the second support 2, first support 1 includes bottom plate 4, baffle 5, reinforcing plate 6 and backup pad 7, bottom plate 4 with one side bottom of baffle 5 links firmly perpendicularly, backup pad 7 with baffle 5 with the perpendicular fixed connection in same one side upper end, reinforcing plate 6 locates the top of baffle 5, backup pad 7 with be connected with a plurality of elastic column 8 between bottom plate 4, a plurality of bar hole 9 has evenly been seted up on backup pad 7, it includes first connecting rod 10 and the second connecting rod 11 of mutual rotation connection to cut formula connecting piece 3, the upper end of first connecting rod 10 with first support 1 tip is articulated, the lower end of the first connecting rod 10 is hinged to the end of the second support 2, the upper end of the second connecting rod 11 is hinged to the end of the second support 2, and the lower end of the second connecting rod is hinged to the end of the first support 1.

In this embodiment, the first support 1 and the second support 2 are preferably identical in size.

In this embodiment, preferably, there are two reinforcing plates 6, and the bottom of the two reinforcing plates 6 is fixedly connected with the same backing plate 12, and the bottom end of the backing plate 12 is provided with anti-slip patterns.

In this embodiment, preferably, the two side edges of the supporting plate 7 are vertically fixed with a limiting plate 13.

In this embodiment, it is preferable that the elastic column 8 includes a fixed sleeve 14, a spring 15, and a sleeve rod 16, a bottom of the sleeve rod 16 extends to an inside of the sleeve 14 and is connected to an upper end of the spring 15, and a lower end of the spring 15 is connected to a bottom of an inside of the sleeve 14.

Preferably, a rubber pad 17 is fixed to the upper end surface of the baffle 5.

It should be noted that, the utility model is a fixing bracket of computer case for aerospace, when in use, the case is clamped and fixed by the first support 1 and the second support 2, the stability of the case is increased, the case is prevented from falling down by external force, the safety of the case is protected, the loss is avoided, meanwhile, a support plate 7 is arranged, the first support 1 and the second support 2 are movably connected by a shear type connecting piece 3, cases with different sizes can be installed according to the adjustment of the distance between the first support 1 and the second support 2, the case is installed on the support plate 7 and can play the function of ventilation and heat dissipation for the bottom of the case, an elastic column 8 is connected between the support plate 7 and a bottom plate 4, when the case is installed on the support plate 7, the weight of the case begins to compress towards the elastic column 8, and further the relative rotation between a first connecting rod 10 and a second connecting rod 11 in the shear type connecting piece 3 is avoided, the bottom end of the backing plate 12 is provided with the anti-slip lines, so that the first support 1 and the second support 2 are ensured not to move any more, the reliability of use and the stability of connection can be improved, the safety of the case is ensured, and the use is more convenient.

The basic principles and the main features of the invention and the advantages of the invention have been shown and described above. It will be understood by those skilled in the art that the present invention is not limited to the above embodiments, and that the foregoing embodiments and descriptions are provided only to illustrate the principles of the present invention without departing from the spirit and scope of the present invention. The scope of the invention is defined by the appended claims and equivalents thereof.

Claims

1. The utility model provides a fixed bolster of computer box for aerospace, includes first support (1) and second support (2), its characterized in that: the first support (1) is movably connected with the second support (2) through a shear type connecting piece (3), the first support (1) comprises a bottom plate (4), a baffle plate (5), a reinforcing plate (6) and a supporting plate (7), the bottom plate (4) is vertically and fixedly connected with the bottom of one side of the baffle plate (5), the supporting plate (7) is vertically and fixedly connected with the upper end of the same side of the baffle plate (5), the reinforcing plate (6) is arranged above the baffle plate (5), a plurality of elastic columns (8) are connected between the supporting plate (7) and the bottom plate (4), a plurality of strip-shaped holes (9) are uniformly formed in the supporting plate (7), the shear type connecting piece (3) comprises a first connecting rod (10) and a second connecting rod (11) which are rotatably connected with each other, the upper end of the first connecting rod (10) is hinged with the end of the first support (1), the lower end of the first connecting rod (10) is hinged to the end of the second support (2), the upper end of the second connecting rod (11) is hinged to the end of the second support (2), and the lower end of the second connecting rod is hinged to the end of the first support (1).

2. The fixing bracket of the computer box for aerospace of claim 1, wherein: the first support (1) and the second support (2) are identical in structure size.

3. The fixing bracket of the computer box for aerospace of claim 1, wherein: the reinforcing plate (6) is provided with two reinforcing plates, the bottom of each reinforcing plate (6) is fixedly connected with the same base plate (12), and the bottom end of each base plate (12) is provided with anti-skid grains.

4. The fixing bracket of the computer box for aerospace of claim 1, wherein: and the edges of two sides of the supporting plate (7) are vertically fixed with limit plates (13).

5. The fixing bracket of the computer box for aerospace of claim 1, wherein: elastic column (8) are including fixed sleeve (14), spring (15) and loop bar (16), the bottom of loop bar (16) extends to sleeve (14) is inboard and with the upper end of spring (15) is connected, the lower extreme of spring (15) with the inboard bottom of sleeve (14) is connected.

6. The fixing bracket of the computer box for aerospace of claim 1, wherein: and a rubber pad (17) is fixed on the upper end surface of the baffle (5).